Pressure Coefficient for Slender Bodies of Revolution Calculator

✖The Angle of Inclination is the angle between a reference plane and the surface of a body, influencing the flow behavior in fluid mechanics.ⓘ Angle of Inclination [θ]			+10% -10%
✖The Curvature of Surface is a measure of how much a surface deviates from being flat, influencing fluid flow behavior in various mechanical applications.ⓘ Curvature of Surface [k_c]			+10% -10%
✖The Distance of Point from Centroidal Axis is the measurement from a specific point to the centroidal axis, important for analyzing fluid flow in hypersonic conditions.ⓘ Distance of Point from Centroidal Axis [y]			+10% -10%

✖The Pressure Coefficient is a dimensionless number that represents the relative pressure difference at a point in a fluid flow compared to the surrounding atmospheric pressure.ⓘ Pressure Coefficient for Slender Bodies of Revolution [C_p]

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Pressure Coefficient for Slender Bodies of Revolution Solution

STEP 0: Pre-Calculation Summary

Formula Used

Pressure Coefficient = 2*(Angle of Inclination)^2+Curvature of Surface*Distance of Point from Centroidal Axis
C_p = 2*(θ)^2+k_c*y
This formula uses 4 Variables

Variables Used

Pressure Coefficient - The Pressure Coefficient is a dimensionless number that represents the relative pressure difference at a point in a fluid flow compared to the surrounding atmospheric pressure.
Angle of Inclination - (Measured in Radian) - The Angle of Inclination is the angle between a reference plane and the surface of a body, influencing the flow behavior in fluid mechanics.
Curvature of Surface - (Measured in Meter) - The Curvature of Surface is a measure of how much a surface deviates from being flat, influencing fluid flow behavior in various mechanical applications.
Distance of Point from Centroidal Axis - (Measured in Meter) - The Distance of Point from Centroidal Axis is the measurement from a specific point to the centroidal axis, important for analyzing fluid flow in hypersonic conditions.

STEP 1: Convert Input(s) to Base Unit

Angle of Inclination: 32 Degree --> 0.55850536063808 Radian (Check conversion here)
Curvature of Surface: 0.2 Meter --> 0.2 Meter No Conversion Required
Distance of Point from Centroidal Axis: 1.2 Meter --> 1.2 Meter No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

C_p = 2*(θ)^2+k_c*y --> 2*(0.55850536063808)^2+0.2*1.2

Evaluating ... ...

C_p = 0.863856475722944

STEP 3: Convert Result to Output's Unit

0.863856475722944 --> No Conversion Required

FINAL ANSWER

0.863856475722944 ≈ 0.863856 <-- Pressure Coefficient

(Calculation completed in 00.004 seconds)

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Created by Sanjay Krishna

Amrita School of Engineering (ASE), Vallikavu

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National Institute Of Technology (NIT), Hamirpur

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< Newtonian Flow Calculators

Exact Normal Shock Wave Maximum Coefficient of Pressure

LaTeX Go Maximum Pressure Coefficient = 2/(Specific Heat Ratio*Mach Number^2)*(Total Pressure/Pressure-1)

Pressure Coefficient for Slender Bodies of Revolution

LaTeX Go Pressure Coefficient = 2*(Angle of Inclination)^2+Curvature of Surface*Distance of Point from Centroidal Axis

Pressure Coefficient for Slender 2D Bodies

LaTeX Go Pressure Coefficient = 2*(Angle of Inclination^2+Curvature of Surface*Distance of Point from Centroidal Axis)

Modified Newtonian Law

LaTeX Go Pressure Coefficient = Maximum Pressure Coefficient*(sin(Angle of Inclination))^2

Pressure Coefficient for Slender Bodies of Revolution Formula

LaTeX Go

Pressure Coefficient = 2*(Angle of Inclination)^2+Curvature of Surface*Distance of Point from Centroidal Axis
C_p = 2*(θ)^2+k_c*y

What is a pressure coefficient?

The pressure coefficient is a dimensionless number which describes the relative pressures throughout a flow field in fluid dynamics.

How to Calculate Pressure Coefficient for Slender Bodies of Revolution?

Pressure Coefficient for Slender Bodies of Revolution calculator uses Pressure Coefficient = 2*(Angle of Inclination)^2+Curvature of Surface*Distance of Point from Centroidal Axis to calculate the Pressure Coefficient, Pressure Coefficient for Slender Bodies of Revolution formula is defined as a measure of the aerodynamic efficiency of slender bodies in hypersonic flow, reflecting the relationship between pressure variations and the body's curvature and angle of attack. Pressure Coefficient is denoted by C_p symbol.

How to calculate Pressure Coefficient for Slender Bodies of Revolution using this online calculator? To use this online calculator for Pressure Coefficient for Slender Bodies of Revolution, enter Angle of Inclination (θ), Curvature of Surface (k_c) & Distance of Point from Centroidal Axis (y) and hit the calculate button. Here is how the Pressure Coefficient for Slender Bodies of Revolution calculation can be explained with given input values -> 0.302148 = 2*(0.55850536063808)^2+0.2*1.2.

FAQ

What is Pressure Coefficient for Slender Bodies of Revolution?

Pressure Coefficient for Slender Bodies of Revolution formula is defined as a measure of the aerodynamic efficiency of slender bodies in hypersonic flow, reflecting the relationship between pressure variations and the body's curvature and angle of attack and is represented as C_p = 2*(θ)^2+k_c*y or Pressure Coefficient = 2*(Angle of Inclination)^2+Curvature of Surface*Distance of Point from Centroidal Axis. The Angle of Inclination is the angle between a reference plane and the surface of a body, influencing the flow behavior in fluid mechanics, The Curvature of Surface is a measure of how much a surface deviates from being flat, influencing fluid flow behavior in various mechanical applications & The Distance of Point from Centroidal Axis is the measurement from a specific point to the centroidal axis, important for analyzing fluid flow in hypersonic conditions.

How to calculate Pressure Coefficient for Slender Bodies of Revolution?

Pressure Coefficient for Slender Bodies of Revolution formula is defined as a measure of the aerodynamic efficiency of slender bodies in hypersonic flow, reflecting the relationship between pressure variations and the body's curvature and angle of attack is calculated using Pressure Coefficient = 2*(Angle of Inclination)^2+Curvature of Surface*Distance of Point from Centroidal Axis. To calculate Pressure Coefficient for Slender Bodies of Revolution, you need Angle of Inclination (θ), Curvature of Surface (k_c) & Distance of Point from Centroidal Axis (y). With our tool, you need to enter the respective value for Angle of Inclination, Curvature of Surface & Distance of Point from Centroidal Axis and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.

How many ways are there to calculate Pressure Coefficient?

In this formula, Pressure Coefficient uses Angle of Inclination, Curvature of Surface & Distance of Point from Centroidal Axis. We can use 2 other way(s) to calculate the same, which is/are as follows -

Pressure Coefficient = 2*(Angle of Inclination^2+Curvature of Surface*Distance of Point from Centroidal Axis)
Pressure Coefficient = Maximum Pressure Coefficient*(sin(Angle of Inclination))^2

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